ARROW AVIATION .::;:nr...,,<>.1"' Run Sheet

REFERENCE ONLY) ENGINE

Turbine

CAE slave

CAC slave

CAG slave

CAT

WORK ORDER# 1 i-818

37784

1197 F

TORO) (CRUISE A)

TOT (F) i 198

TORO. 243.3

66.9

N1 93

/\12 (RPM)- 6017

INLET PRES. 30.24

INLET TEMP. 58

FUEL FLOW R] 121.2

COMP. VENT 0

G.B. PRESSURE 0 72

VIBRATION (IPS)

GEAR BOX

TURBINE

ENGINE TORQUE CHECK

CAL.TORQ{PSl) 67.2

PS! D!FF i .8) 03

1286 F TORO)

{CRU

1288

290

79.2

96.1

001�

30.24

58

218.3 0

0 81

0.9

1360 F 1434 F 1490 F (349 TOHO.) (366

(5 MIN.)

1336 1393 1415

324.6 351.2 367

90.6 97. 1 102.7

98.1 99.9 100.5

.---@GOO . - -&:l31 Sf:t2B

30.24 30.24 30.24

57 58 58

235 2495 260 0 0 0

0 0 0 88 90 90

897 97.0 1014

·O.i

TOT COR. FACT{T5) 1.00210

HP COR FACT(SHP) 0.99037

FUEL C.F.(W2) 0.99169

OBSERVED HP 278.7

COR. TOT (F) 1201 COR HP (SHP) 276.1 SPEC.FUEL 0.43539

(LB/HP/HR)

278 1197 F

COA. HP (SHP) 273.4 %01FF. -1.6

SPEC.FUEL 0.893 %DIFF. 26.1

- ------ - .

-· ---- - -- - ---lr.ffl8 - ..

1.00210

0.99037

0.99169

331.9

1292 328J

0.65858

333 1286 F

325.4 -2.3

0.598 -10.0

---o.665 -

1.00415 1.00210 1.00210

0.99135 0.99037 0.99037

0.99317 0.99169 0.99169

371.3 403.3 421.2

1343 1397 1419 368.1 399.4 417.2

0.63403 0.61948 0.61806

370 400 420 1360 F 1434F

377.8 429.3 2.1 7.3

0.630 0.617 -3.2 -5.6 - - 0:65 -- ---

----u�os ·······------------------ ····--- ····------ . . . . I

j SEA LEVEL CALIBRATION C20

500.0 450.0 400.0 350.0

a..: 300.0 ::r: a: 250.0 0 200.0 0

150.0 .. 100.0

50.0 . 0.0

1197 1286 F F

1360 F 1434 F

COR. TOT

-+-ENGINE SHP

···"*··-SPEC. SHP I ! !

)

)

I 1

' PHI 250T1 (5/95)

SERVICE RECORD

TURBINE ASSEMBLY Part I

Page No.

®

Turbine Serial Number_C_A_T_..:- 3�?.....!7�9�4=-------- Engine Model_25 _o- _C ..:::;;J.�o:;..:Jt:::.._ _____ :.....:.__

INSTALLED REMOVED

Aircraft SIN TT

Engine S/N Date Date Reason

r PHI 250T2 (5195) TRANSFER RECORD

Partll C:�J)·

Turbine Serial Number .....;:;c;...:. AT.:.....- .-..:;:3;.....7:....7wK��....._<I _____ _

TRANSFERRED/SHIPPED

I I I

Date From To I

Page No. ,"). ----

Engine Model =25:..::. 0_- !...i..({�KJ;,!;:;8 :..__ ______ _

RECEIVED Turbine Time

I Total I Since OH Date Organization

\ ,,

,(

. '

,.

,.

)

4VI4LLli -® MODIFICATION RECORD Part Ill

A IIWMa SYWI'III Company

TURBINE ASSEMBLY Page No. 6

Turbine Serial Number 0A-T 31) tY Engine Model ;)5]) --coO�

Compliance Date

A-3A042·6 R6-89

Bulletin or Directive No.

MODIFICATION RECORD Part Ill

TURBINE ASSEMBLY Page No. �

Turbine Serial Number tAT 37)/ ¥ Engine Model ,;;>sJ -C()f) 0

Compliance Date

Bulletin or Directive No. Title

FORM 27830 (11-n) MODIFICATION RECORD

TURBINE ASSEMBLY

Pert Ill PageNo. t'J --=----

Turbine Serial Number _C .... Ac...f.a.;_· -=3'--7._'7.:....;9::::...t/..L.------ Engine Model <15 o · c �B

Title Signature Organization

FORM 27830 (11-n) MODIFICATION RECORD

TURBINE ASSEMBLY

Part Ill b Page No. __ o __ _

Turbine Serial Number --.:Di::1..!..1-1=-- ·�3...t..7...t..7-�.6'L.:/J.._ _____ _ Engine Model ---=:;&.:..::5::...;0:.....·-=Cd.�cffi!.J._ ___ _

Bulletin or Trtle Signature Organization Directive No.

'8

Part IV Page No. __._'7 _

INSPECTION-MAINTENANCE-OVERHAUL RECORD FORM 27840 (11-n) TURBINE ASSEMBLY

) Turbine Serial Number f:.a =r- .311 8 '-} Date

,

Remarks

Engine Model �5o-Cr&o'O

Signature Organization

Part IV PageNo. 8

INSPECTION-MAINTENANCE-OVERHAUL RECORD

FORM 27840 (11-77) TURBINE ASSEMBLY

Turbine Serial Number te r· 31 '7 9 t-f Engine Model dl5o - C.Pl.CB

Date Remarks Signature Organization

1. Approving National Aviation 2. 3. Form Tracking Number: Authority/Country:

AUTHORIZED RELEASE CERTIFICATE 11-818-400 FAA/UNITED STATES

FAA Form 8130-3, AIRWOR11IINESSAPPROV AL TAG 4. Organization Name and Address: 5. Work Order/Contract/Invoice

Number: ARROW AVIATION CO., LLC 1318 SMEDE HIGHWAY BROUSSARD LA 70518 FAA CERTIFIED REPAIR STATION #Y3ARS27Y 11-818

6. Item: 7. Description: 8. Part Number: 9. Eligibility:* 10. Quantity: 11. Serial/Batch Number: 12. Status/Work:

1 Turbine Assembly 23038241 N/A 1 CAT-37784 REPAIR

13. Remarks: Repaired Turbine S/N CAT -37784 TT 12031.35 TSO 419.10 due to containment ring modification and performed turbine part of 150 and 300 hour inspection. All work was done I.A. W. Rolls Royce

M250/C20 Overhaul Manual 1 OW3 4th edition 8th revision dated 8-15-12, Opeation and Maintenance Manual 1 OW2 6th edition 16th revision dated 6-1-11.

1 • rtifies the items identified above were manufactured in conformity to: 19. [g) 14 CFR 43.9 Return to Service 0 Other regulation specified in Block 13

0 Appro esign data and are in condition for safe operation. Certifies that unless otherwise specified in block 13, the work identified in Block 12

0 Non-approved de - data specified in Block 13. and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

15, Autbori•od s;gnotu� 16. Approval/Authorization No.: 20. Authorized Signature: 21. Approval/Certificate No.:

� CRS#: Y3ARS27Y

� �DAVY\alY\ �rintod)' 18. Date:

� 22. Nametfyped or Printed): 23. Date (m/d!y):

Coby Johnson 10-18-12

U ser/lnstaller Responsibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness accepts parts/components/assemblies from the airworthiness authority of the country specified in Block!.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) *Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005